EPFD-02-06 Technical Measures of Effectiveness-Rev B .pdf

PDF 1 MB Posted

Attached to
Electrified Powertrain Flight Demonstration Federal contract opportunity
Solicitation number
80AFRC21R0009
Issued by
National Aeronautics and Space Administration Armstrong Flight Research Center

About this file

This technical document outlines measures for evaluating an electrified aircraft powertrain demonstration project. Key performance parameters include metrics for power density, efficiency, and specific power. Measures of effectiveness will assess achievement of strategic technology goals for energy efficiency and reduced emissions. Technical performance measures are aligned with objectives for subsonic transport electrification. Validation methods incorporate ground and flight tests to evaluate the powertrain system against defined metrics.

The related federal contract opportunity notice announces NASA Armstrong Flight Research Center's intent to solicit proposals for an "Electrified Powertrain Flight Demonstration" program. The program aims to develop, test, and demonstrate a megawatt-class electrified aircraft powertrain system through multiple award contracts. Interested offerors should monitor the Federal Business Opportunities website for release of a potential request for proposal.

View the file

Other files for this federal contract opportunity

Other files attached to Electrified Powertrain Flight Demonstration, newest first.
File Type Posted
Domestic or Foreign End Product - Components.xlsx XLSX spreadsheet
80AFRC21R0009P00003.pdf PDF
EPFD-01-03 Integrated Data Requirements Description Document.pdf PDF
EPFD-01-03 Integrated Data Requirements Description Document.pdf PDF
TE-02 Worksheet in EPFD-01-03.xlsx XLSX spreadsheet
TE-03 Worksheet in EPFD-01-03.xlsx XLSX spreadsheet
AFOP-7900.3-023.pdf PDF
AFOP-8730.5-007-2.pdf PDF
Industry Day Presentation.pdf PDF
80AFRC21R0009P00002.pdf PDF
Industry Day Questions and Answers.pdf PDF
AFOP-8715.3-005-2.pdf PDF
80AFRC21R0009P00001.pdf PDF
EPFD-01-03 Integrated Data Requirements Description Document Final.pdf PDF
EPFD-02-02 System Requirements Document.pdf PDF
80AFRC21R0009.pdf PDF
EPFD Statement of Objectives.pdf PDF
EPFD-02-06 Technical Measures of Effectiveness.pdf PDF
EPFD_01_03_Integrated Data Requirements Description Document.pdf PDF
EPFD Industry Day-Public Webinar QAs.pdf PDF
EPFD Industry Day QAs.pdf PDF
EPFD Public Webinars December 11_2020_final__updated_12_15_2020.pdf PDF
EPFD Pre-solicitation Industry Day Slides Final 12.10_with all updates_12_15_2020pptx.pdf PDF
Draft_EPFD Programmatic Data Requirement Deliverables.pdf PDF
Small Business Subcontracting Goals.pdf PDF
Draft_EPFD Technical Data Requirement Deliverables.pdf PDF
EPFD_02_02_SRD-DRAFT-REV A-20201130.pdf PDF
Draft EPFD-02-06 Technical Measures of Effectiveness Preliminary.pdf PDF
DRAFT Statement of Objectives.pdf PDF
DRAFT RFP 80AFRC21R0009.pdf PDF
Notice of Contract Action.pdf PDF
Show all 31

On GovTribe

Work with this file on GovTribe

  • Download the original file
  • Contacts named in this file
  • Similar government files
  • Ask GovTribe AI about this file

Text version

EPFD-02-06 Rev B

Uncontrolled when printed. The electronic version is the official approved document.

National Aeronautics and Space Administration

Electrified Powertrain Flight Demonstration Project

(EPFD)

Technical Measures of Effectiveness

Date: March 23, 2021

EPFD Technical Measures of Effectiveness

Document No: EPFD-02-06 Rev B Effective Date: March 23, 2021 Page iv

Uncontrolled when printed. The electronic version is the official approved document.

TABLE OF CONTENTS

1.0 INTRODUCTION

1.1 Applicable Documents

1.2 Reference Documents

2.0 TECHNICAL MEASUREMENT

2.1 Measures Of Effectiveness (MOE)

2.2 Key Performance Parameter (KPP)

2.3 Measures of Performance (MOP)

2.4 Technical Performance Measures (TPM)

3.0 VALIDATION APPROACH

APPENDIX A ACRONYMS

List of Figures

Figure 1- Integrated MW-class powertrain boundary Figure 2- Relationship of the Technical Measures Figure 3- Demonstration by Analysis Framework

List of Tables

Table 1 - ARMD Strategic Thrust 3 and Critical Commitment 3.1 Table 2 - List of Applicable Documents Table 3 - List of Reference Documents Table 4 – EPFD Measures of Effectiveness Table 5 - Integrated MW-Class Powertrain KPPs Table 6 – EPFD Measures of Performance Table 7 - Integrated MW-Class Powertrain TPMs Table 8 - List of Acronyms

Effective Date: March 23, 2021 Page 3 class powertrain system” on one notional system configuration. An analogous boundary should be defined for the actual system configuration under consideration. Typical components included are electric Machines, inverters, converters, energy storage, circuit protection devices, switches, cables, and connectors.

Figure 1- Integrated MW-class powertrain boundary

Technical Measurements are the set of measurement activities used to provide insight into the progress in the definition and development of the technical solution, ongoing assessment of the associated risks and issues, and the likelihood of meeting the critical objectives of the stakeholder.

Technical Measurements establish a set of measures based on the expectations and requirements that will be tracked and assessed to determine overall system effectiveness and stakeholder satisfaction. These technical measures include: Measures Of Effectiveness (MOEs), Key Performance Parameters (KPPs), Measures Of Performance (MOPs), and Technical Performance Measures (TPMs). The project stakeholders are defined in EPFD-01-01 Preliminary Project Plan.

There interdependent relationships are seen in Figure 2 below. Measures Of Effectiveness (MOEs) and will track progress against the stakeholder’s needs and expectations. Key Performance Parameters (KPPs) flow from the MOEs in the context of a Vision Vehicle. The MOPs flow from the MOEs. The EPFD technical measures will be used track progress of individual flight demonstration efforts conducted within the project.

Effective Date: March 23, 2021 Page 8 performance of the Vision Vehicle against the ARMD Subsonic Transport Level Metrics. The flow of TPMs to KPPs up to the ARMD Subsonic Transport Level Metrics is shown in Figure 3.

Figure 3- Demonstration by Analysis Framework

File details come from the government source that posted it. Updated .